Shaft hole cooling and lubrication system

A cooling lubrication and shaft hole technology, applied in the field of cooling and lubrication, can solve the problems of difficulty in meeting the requirements of the micro power generation system in the aviation field, the limited space of the micro high-speed generator, and the increase of the size and weight of the generator, so as to achieve a simple structure and improve the cooling effect. , The effect of reducing the difficulty of processing
CN105162286BActive Publication Date: 2018-01-09SHENYANG AEROSPACE XINGUANG GRP

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
SHENYANG AEROSPACE XINGUANG GRP
Publication Date
2018-01-09

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Abstract

The invention relates to a shaft hole cooling and lubricating system, which is composed of an internal circulating oil circuit and an external oil circuit. The internal circulating oil circuit includes an oil pump, a lubricating oil tank, a rotary static joint, and a rotating shaft; the external oil circuit includes a cooling jacket, an oil pump, Main fuel tank: Compared with other cooling and lubricating systems, the device of the present invention has the characteristics of simple structure and few parts, which is easy to realize processing, can greatly reduce the thickness of the outer case and the space of the generator, and reduce the weight of the system ; Reduce processing difficulty; and this device adopts double oil circuit structure, the effect of cooling and lubricating is obvious.
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Description

technical field

[0001] The invention relates to a shaft hole cooling and lubricating system for cooling and lubricating a high-speed generator in a microturbine power generation system. Its technology belongs to the field of cooling and lubrication, and can be used for cooling and lubrication of miniature high-speed power generation systems in the aerospace field that are sensitive to weight and size and have serious heat generation. Background technique

[0002] In the field of aerospace, microturbine power generation systems have relatively strict restrictions on space and weight. Because the high-speed and high-power power generation system will generate a lot of heat during the working process; in the micro-ram turbine power generation system, in order to save space and weight, the distance between the generator and the turbine is relatively close, and a large amount of heat in the turbine will be transferred to the generator; At the same time, the continuous and stable...

Claims

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